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Inconel 617 丝材 UNS N06617/NiCr22Co12Mo9 / NS3106/ 2.4663

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Inconel 617 Wire (UNS N06617 / NiCr22Co12Mo9 / NS3106 / 2.4663) is a nickel-based solid-solution-strengthened alloy. With excellent high-temperature resistance, oxidation resistance, and corrosion resistance, it serves as a critical material in extreme environments.

 

Inconel 617 (UNS N06617)
Chemical Composition (%) Ni ≥ 44.5 Cr: 20.0-24.0
Mo: 8.0-10 Fe ≤ 3.0
Mn ≤ 1.0 C: 0.05-0.15
Si ≤ 1.0 Al: 0.8-1.5
Ti ≤ 0.6 Co: 10.0-15.0
Melting Point (℃) 1330-1380
Density (g/cm³) 8.4
Application Areas Inconel 617 is regarded as a premier material for offshore oil and gas extraction equipment, such as offshore pipelines. Using Inconel 617 in high-speed rotating components like aero-engines and gas turbines significantly enhances fatigue resistance and high-temperature performance, ensuring long-term stable operation.
Below is the core information:

1. Chemical Composition

The typical chemical composition of Inconel 617 is (%):
  • Nickel (Ni): ≥ 44.5
  • Chromium (Cr): 20-24
  • Cobalt (Co): 10-15
  • Molybdenum (Mo): 8-10
  • Aluminum (Al): 0.8-1.5
  • Iron (Fe): ≤ 3.0
  • Titanium (Ti): ≤ 0.6
  • Carbon (C): 0.05-0.15
  • Others: Trace elements such as silicon, manganese, sulfur, etc.
Role of Key Elements:
  • Chromium: Enhances resistance to oxidation and sulfide corrosion.
  • Aluminum: Forms a dense oxide film (Al₂O₃), improving high-temperature oxidation resistance.
  • Cobalt and Molybdenum: Improve high-temperature strength through solid-solution strengthening.

2. Core Properties

  1. High-Temperature Resistance
    • Operating Temperature: -196°C to 1100°C, with short-term tolerance up to 1150°C.
    • High-Temperature Strength: Maintains approximately 80% of room temperature tensile strength (approx. 800 MPa) at 600°C, with excellent creep resistance.
  2. Corrosion Resistance
    • Oxidation Resistance: Rapidly forms a protective oxide film at high temperatures, resisting oxidation and carburization.
    • Medium Corrosion Resistance: Exhibits good tolerance to nitric acid, chlorides, seawater, and sulfur-containing environments, with outstanding performance in sulfide environments.
  3. Mechanical Properties (Room Temperature)
    • Tensile Strength: ≥ 690 MPa
    • Yield Strength (0.2%): ≥ 310 MPa
    • Elongation: ≥ 30%
    • Hardness: ≤ 220 HB

3. Application Areas

  • Energy Industry:
    • Gas turbine combustion chambers, turbine blades, transition pieces.
    • Heat exchangers for nuclear high-temperature gas-cooled reactors, nuclear reactor components.
    • Flue gas desulfurization equipment for coal-fired power plants.
  • Chemical & Petrochemical:
    • Nitric acid production catalyst supports, high-temperature reactors, coil tubes.
    • Molybdenum refining equipment.
  • Aerospace:
    • Aero-engine gas turbine components, combustion chamber casings.
  • Heat Treatment:
    • High-temperature furnace muffle tanks, radiant tubes, heating elements.

4. Machining and Welding

  1. Hot Working
    • Hot Forming Temperature: 1200-950°C. High-power equipment is required to avoid grain coarsening.
    • Solution treatment (1120-1200°C) followed by water quenching or air cooling is required after forming.
  2. Cold Working
    • High work hardening rate; intermediate annealing (approx. 870°C) is required.
    • Solution treatment is required after cold forming to restore plasticity.
  3. Welding
    • TIG or MIG welding is recommended using ENiCrMo-3 filler wire.
    • Clean the surface before welding to avoid contaminants affecting corrosion resistance.

5. Standards and Certifications

  • International Standards:
    • ASTM B166 (Bar), ASTM B564 (Forgings), AMS 5887 (Bar / Forgings), AMS 5888 (Plate).
    • ISO 6208 (Plate), DIN 17750 (Plate), VDTÜV 485 (Comprehensive Standard).

6. Precautions

  • Hot Working Control: Avoid dwelling in the sensitive temperature range of 900-1000°C to prevent grain coarsening.
  • Surface Treatment: Scale can be removed by pickling or sandblasting to enhance corrosion resistance.
  • Environmental Adaptability: Avoid contact with molten metals (e.g., lead, zinc) to prevent hot brittleness.

7. Comparative Advantages

Material Advantages Limitations
Inconel 617 Excellent high-temperature strength and sulfide corrosion resistance Higher difficulty in cold working
Inconel 625 Better weldability, resistant to chloride ion corrosion Slightly lower high-temperature strength
Hastelloy C-276 Resistant to reducing acid corrosion Insufficient high-temperature strength

Summary

Inconel 617, leveraging its high nickel-chromium-cobalt-molybdenum alloy characteristics, excels in extreme high-temperature, high-pressure, and corrosive environments. It is a critical material in aerospace, energy, and chemical industries. Its stringent manufacturing processes and international certifications ensure long-term reliability, making it particularly suitable for cutting-edge applications such as Generation IV nuclear power systems and advanced gas turbines.

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